Active and Passive Flow Control in a Turbine Cascade

R.K. Sullerey,; Alok Mishra,

doi:10.1515/TJJ.2008.25.3.155

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Active and Passive Flow Control in a Turbine Cascade

R.K. Sullerey, und Alok Mishra,

Veröffentlicht/Copyright: 1. September 2008

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Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 25 Heft 3

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Chicago
Vancouver

Sullerey,, R.K. and Mishra,, Alok. "Active and Passive Flow Control in a Turbine Cascade" International Journal of Turbo and Jet Engines, vol. 25, no. 3, pp. 155-162. https://doi.org/10.1515/TJJ.2008.25.3.155

Sullerey,, R. & Mishra,, A. (). Active and Passive Flow Control in a Turbine Cascade. International Journal of Turbo and Jet Engines, 25(3), 155-162. https://doi.org/10.1515/TJJ.2008.25.3.155

Sullerey,, R. and Mishra,, A. () Active and Passive Flow Control in a Turbine Cascade. International Journal of Turbo and Jet Engines, Vol. 25 (Issue 3), pp. 155-162. https://doi.org/10.1515/TJJ.2008.25.3.155

Sullerey,, R.K. and Mishra,, Alok. "Active and Passive Flow Control in a Turbine Cascade" International Journal of Turbo and Jet Engines 25, no. 3 (): 155-162. https://doi.org/10.1515/TJJ.2008.25.3.155

Sullerey, R, Mishra, A. Active and Passive Flow Control in a Turbine Cascade. International Journal of Turbo and Jet Engines. ;25(3): 155-162. https://doi.org/10.1515/TJJ.2008.25.3.155

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Artikel in diesem Heft

CONTENTS
Reduced-Order Model of a Mistuned Multi-Stage Bladed Rotor
Active and Passive Flow Control in a Turbine Cascade
Effects of Geometric and Structural Parameters on Coupled Bending Torsion Flutter in Turbo Machinery Blades
Turbomachine Shrouded Rotor Blade Forced Response Analysis
Numerical Investigation on Multi-cycle Operation of Pulse Detonation Rocket Engine
Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine
Performance Improvement of Gas Turbine Cycles
Characteristics of Supersonic Impinging Moist Air Jets

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https://doi.org/10.1515/TJJ.2008.25.3.155

Artikel in diesem Heft

CONTENTS
Reduced-Order Model of a Mistuned Multi-Stage Bladed Rotor
Active and Passive Flow Control in a Turbine Cascade
Effects of Geometric and Structural Parameters on Coupled Bending Torsion Flutter in Turbo Machinery Blades
Turbomachine Shrouded Rotor Blade Forced Response Analysis
Numerical Investigation on Multi-cycle Operation of Pulse Detonation Rocket Engine
Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine
Performance Improvement of Gas Turbine Cycles
Characteristics of Supersonic Impinging Moist Air Jets